Tomasz Rybus

Tomasz Rybus


Research Focus & Metrics

Academic Career Length

15Years (2012-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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8 July 2016 in Journal of Intelligent & Robotic Systems
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Journal Article
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TRTomasz Rybus
Tomasz Rybus
KSKarol Seweryn
Karol Seweryn
JSJurek Z. Sasiadek
Jurek Z. Sasiadek

1 August 2018 in Progress in Aerospace Sciences
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Journal Article
Closed access
TRTomasz Rybus
Tomasz Rybus

1 January 2022 in Acta Astronautica
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Journal Article
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TRTomasz Rybus
Tomasz Rybus
MWMateusz Wojtunik
Mateusz Wojtunik
FBFatina Liliana Basmadji
Fatina Liliana Basmadji

1 February 2019 in Acta Astronautica
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Journal Article
Closed access
TRTomasz Rybus
Tomasz Rybus
KSKarol Seweryn
Karol Seweryn
JOJakub Oleś
Jakub Oleś
FBFatina Basmadji
Fatina Basmadji
KTKamil Tarenko
Kamil Tarenko
PWPiotr Wolanski
Piotr Wolanski

24 July 2019 in Robotica
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Journal Article
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TRTomasz Rybus
Tomasz Rybus
SUMMARY: It is usually proposed to use a robotic manipulator for performing on-orbit capture of a target satellite in the planned active debris removal and on-orbit servicing missions. Control of the satellite-manipulator system is challenging because motion of the manipulator influences position and orientation of the chaser satellite. Moreover, the trajectory selected for the capture manoeuvre must be collision-free. In this article, we consider the case of a nonredundant manipulator mounted on a free-floating satellite.We propose to use the bi-directional rapidly-exploring random trees (RRT) algorithm to achieve two purposes: to plan a collision-free manipulator trajectory that, at the same time, will result in a desired change of the chaser satellite orientation. Several improvements are introduced in comparison to the previous applications of the RRT method for manipulator mounted on a free-floating satellite. Feasibility of the proposed approach is demonstrated in numerical simulations performed for the planar case in which the chaser satellite is equipped with a 2-DoF (Degree of Freedom) manipulator. The obtained results are analysed and compared with the results obtained from collision-free trajectory planning methods that do not allow to set the desired final orientation of the chaser satellite.